In 1942 Dawydoff obtained the plans and the rights to produce the Slingsby Cadet under licence from Fred Slingsby. Dawydoff had the plans redrawn to US measurements, the structural strength increased, plus a new tow hook and wing rigging design. The wing is assembled using just one 4 ft (1.2 m) long pin per wing.
The UT-1 is built predominantly from wood, with the fuselage wooden framed and covered in plywood. The wing and tail are also wooden-framed and covered in doped aircraft fabric covering. The two-spar wing is supported by dual struts.
Dawydoff's plan was to gain government support to provide the UT-1 in kit form for assembly by schools and clubs. The government money was not forthcoming and the post-war period saw a large number of surplus military training gliders saturate the market. As a result, only one UT-1 was completed. It is now located in the National Soaring Museum.
Specifications
General characteristics
Crew: one Wingspan: 38 ft 5 in (11.71 m) Wing area: 172.5 sq ft (16.03 m2) Aspect ratio: 8.5:1 Airfoil: Go 426 Empty weight: 276 lb (125 kg) Gross weight: 450 lb (204 kg)
Performance
Maximum glide ratio: 14.7:1 at 30 mph (48 km/h) Rate of sink: 210 ft/min (1.1 m/s) at 28 mph (45 km/h) Wing loading: 2.6 lb/sq ft (13 kg/m2)